Body-axis rolling motion critical states of a 65-degree delta wing
- 11 January 1993
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Roll-induced cross-loads on a delta wing at high incidencePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Simplification of nonlinear indicial response models - Assessment for the two-dimensional airfoil caseJournal of Aircraft, 1991
- Large-amplitude high-rate roll oscillation system for the measurement of non-linear airloadsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Large-amplitude high-rate roll experiments on a delta and double delta wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990